IL97246A - Non-interfering viewing system for use in catadioptric projection systems - Google Patents

Non-interfering viewing system for use in catadioptric projection systems

Info

Publication number
IL97246A
IL97246A IL9724691A IL9724691A IL97246A IL 97246 A IL97246 A IL 97246A IL 9724691 A IL9724691 A IL 9724691A IL 9724691 A IL9724691 A IL 9724691A IL 97246 A IL97246 A IL 97246A
Authority
IL
Israel
Prior art keywords
viewer
image
radiance
nanometers
viewing
Prior art date
Application number
IL9724691A
Other languages
Hebrew (he)
Other versions
IL97246A0 (en
Original Assignee
Hughes Aircraft Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Hughes Aircraft Co filed Critical Hughes Aircraft Co
Publication of IL97246A0 publication Critical patent/IL97246A0/en
Publication of IL97246A publication Critical patent/IL97246A/en

Links

Classifications

    • GPHYSICS
    • G09EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
    • G09BEDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
    • G09B9/00Simulators for teaching or training purposes
    • G09B9/02Simulators for teaching or training purposes for teaching control of vehicles or other craft
    • G09B9/08Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer
    • G09B9/30Simulation of view from aircraft
    • G09B9/32Simulation of view from aircraft by projected image
    • G09B9/326Simulation of view from aircraft by projected image the image being transformed by optical means
    • GPHYSICS
    • G02OPTICS
    • G02BOPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B27/00Optical systems or apparatus not provided for by any of the groups G02B1/00 - G02B26/00, G02B30/00
    • G02B27/01Head-up displays
    • G02B27/0101Head-up displays characterised by optical features
    • GPHYSICS
    • G09EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
    • G09BEDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
    • G09B9/00Simulators for teaching or training purposes
    • G09B9/003Simulators for teaching or training purposes for military purposes and tactics
    • GPHYSICS
    • G02OPTICS
    • G02BOPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B27/00Optical systems or apparatus not provided for by any of the groups G02B1/00 - G02B26/00, G02B30/00
    • G02B27/01Head-up displays
    • G02B27/0101Head-up displays characterised by optical features
    • G02B2027/0118Head-up displays characterised by optical features comprising devices for improving the contrast of the display / brillance control visibility
    • G02B2027/012Head-up displays characterised by optical features comprising devices for improving the contrast of the display / brillance control visibility comprising devices for attenuating parasitic image effects
    • GPHYSICS
    • G02OPTICS
    • G02BOPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B27/00Optical systems or apparatus not provided for by any of the groups G02B1/00 - G02B26/00, G02B30/00
    • G02B27/01Head-up displays
    • G02B27/0179Display position adjusting means not related to the information to be displayed
    • G02B2027/0187Display position adjusting means not related to the information to be displayed slaved to motion of at least a part of the body of the user, e.g. head, eye
    • GPHYSICS
    • G02OPTICS
    • G02BOPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B5/00Optical elements other than lenses
    • G02B5/20Filters
    • G02B5/28Interference filters

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Theoretical Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Educational Technology (AREA)
  • Educational Administration (AREA)
  • Business, Economics & Management (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Optics & Photonics (AREA)
  • Devices For Indicating Variable Information By Combining Individual Elements (AREA)
  • Stereoscopic And Panoramic Photography (AREA)
  • Projection Apparatus (AREA)
  • Diffracting Gratings Or Hologram Optical Elements (AREA)

Description

NON-INTERFERING VIEWING SYSTEMS FOR USE IN CATADIOPTRIC PROJECTION SYSTEMS. yivwivi! njnpn niDTyna E/IOK/ mmynn ]I-> V παρκ/π ni_nyn HUGHES AIRCRAFT COMPANY C: 12117 97246/2 NON-INTERFERING VIEWING SYSTEMS FOR USE IN CATADIOPTRIC PROJECTION SYSTEMS BACKGROUND OF THE INVENTION 1. Field of the Invention This invention relates to non-interfering viewing systems for use in catadioptric projection systems by two or more persons simultaneously viewing displays in such systems . 2. Description of Related Art Until now, catadioptric area-of-interest display projectors and projection systems have utilized substantially the same displays for simultaneous viewing by two or more persons. A need has developed to provide independent, non-interfering, simultaneous area-of-interest displays for two or more persons.
SUMMARY OF THE INVENTION This invention provides non-interfering area-of-interest display viewing means for two or more persons, hereafter sometimes called viewer No. 1 and viewer No. 2, simultaneously looking at two or more different displays, hereafter sometimes called display No. 1 and display No. 2, within a single catadioptric projection system. Such viewing means permit each of two such persons to see only one of two simultaneous displays without interference from the other display.
The viewing means for each person includes means for determining the line of sight for each viewing means, including means for generating a signal representing the viewer's line of sight, and means for delivering a signal to means in a catadioptric area-of-interest projection system for steering a desired display into the field of view of the viewing means. The viewing means also includes means for transmitting desired wavelengths of light from the desired display, and for rejecting unwanted wavelengths of light, particularly those wavelengths of light intended for another viewer.
More generally, the greater the separation between the desired wavelength of light images intended for viewing by a first viewer, and the desired wavelength of light images intended for viewing by a second viewer, the better the suppression of cross-talk between the two sets of images. For example, if viewer No. 1 is intended to see images having a wavelength of 815 nanometers, and viewer No. 2 is intended to see images having a wavelength of 750 nanometers, the suppression of cross-talk can be about 10,000 to 1 (optical density = 4) . If the longer wavelength is 840 nanometers, instead of 815 nanometers, and the shorter wavelength is 715 nanometers, then the suppression could be about 100,000 to 1 (optical density = 5) . The greater the suppression of cross-talk, the better that the results are. In practice, the gap between the two. wavelengths used, where there are two viewers, for example, depends on the capacities of the optical systems used to produce the images. For the viewing means of this invention, the range of wavelengths from which the images for each of the viewers is selected is preferably from about 600 nanometers to about 1,100 nanometers.
In preferred embodiments, the viewing means comprises selective light-transmitting means adapted to be positioned over a viewer's eyes or viewing aids in the path of light from the desired display. Such light-transmitting means transmit substantially all radiance at the desired wavelength, and reflect or absorb all other wavelengths. In some embodiments, for viewer No. 1, a filter such as a Schott RG830 plate, transmits substantially all radiance at 880 nanometers, and rejects or absorbs substantially all radiance at 750 nanometers, over a field of view subtending an angle in the range of about -20° to about +20°.
For viewer No. 2, a filter such as a.Sinott holographic optical element (HOE) , double holographic optical element or multi-layer thin film filter absorbs or reflects substantially all radiance at 880 nanometers over a field of view subtending an angle in the range of about -20° to about +20°, and transmits all radiance at 750 nanometers. Such filters are of known kinds. The thin film filter can be, for example, a 43-layer stack of alternating Ta205 and SiO,, layers, each of one-quarter wave thickness, with the exception of the first three layers and the air interface layer. 97246/2 BRIEF DESCRIPTION OF THE DRAWINGS The invention can better be understood by reference to the drawings, in which: FIG. 1 is a graph showing the spectral response of a preferred embodiment for a first viewer's light filter; FIGS. 2a and 2b include two graphs showing, for a second viewer, the angular response using single and double holographic optical elements; FIG. 3 shows the spectral response for the two viewers' filters and displays the spectral response of generation 3 night vision goggle (NVG) viewing aids; and FIG. 4 is a schematic diagram showing the simultaneous viewing of two different sets of images by two different viewers in which cross-talk between the two sets is minimized.
DETAILED DESCRIPTION OF THE INVENTION FIG. 1 shows graphically the performance of several different infrared-transmitting filters that transmit substantially all radiance at 880 nanometers wavelength, and rejects or absorbs all radiance at 750 nanometers wavelength, i.e., RG780, RG830 and RG850.
FIGS. 2a and 2b show the estimated optical density versus field of view of single and double holographic optical element (HOE) light filters for a second viewer.
As shown in FIG. 3, the second viewer's filter transmit substantially all radiance at 750 nanometers wavelength, and 97246/2 - 5 -rejects or absorbs substantially all radiance at 830 nanometers wavelength.
In preferred embodiments, dichromated gelatin-based holographic elements (DCG) are useful for display and filter purposes because of their low scattering properties and their high index modulations. DCG holographic filters as thick as 80 microns and with phase gratings having an index modulation of about 0.06 are particularly useful.
Holographic infrared filter elements are preferably either single-layer or double-layer elements. The single-layer element is simpler because it utilizes only one hologram. The double-layer element uses two complementary gratings, one for each of the two field angle ranges, i.e., high and low. In such devices, the angular bandwidth requirements for each element is reduced.
A single-layer hologram filter designed to cover a field of view of about ±20° with a maximum optical density of 4 at 880 nanometers has the following characteristics: thickness (t) of about 45 microns, grating spacing (L) of about 894.5 nanometers and index modulation of about .053. FIG. 2a shows the optical density plotted against input angle, measured in degrees, in air, at 880 nanometers, for randomly polarized light from a single holographic optical element filter. The curve is symmetric about 0°, and thus describes the extinction properties over the entire 40° field. Theoretical transmission for the same hologram at 750 nanometers, neglecting scattering and absorptive losses, exceeds 95% over the same range.
With double-layer holographic filters, the angular coverage requirement is divided between the two elements. One hologram covers the range from about 0° to about 17°, and the second hologram covers the range from about 15° to about 24°. FIG. 2b represents a composite of the two HOE, filter layers. The lump in the curve at incidence angles near 16 is due to overlap in the coverage between the two holograms. As FIG. 2b shows, the associated parameters are less stringent than in the single element case. Thus, the thickness of each hologram can be about 35 microns. The grating spacings are 887 nanometers, and 906 nanometers.
The modulation indices are about .045.
With double-layer filter holograms, each hologram can be thinner than a single-layer filter. Each can have lower modulation requirements. Further, angular coverage at the minimum optical density of 3 is about a 48° theoretical field of view, allowing for inherent spatial inhomogenei-ties. As a result, such filters are more easily produced than single-layer filters, and at lower cost. With the double-layer filters, a contrast ratio of 10,000 to 1 is attainable over the required 40° theoretical field of view.
FIG. 3 shows the use of two different . light filters by two different viewers, such that each viewer sees a display intended only for him without seeing a simultaneous display intended for another viewer within the 97246/2 same catadioptric area-of-interest projection system. The spectral response of a generation 3 night viewing goggle (NVG) viewing aid is typically from 600 to 1,000 nanometers. Hence, the wavelengths selected for each of the two viewers should be within this wavelength range.
FIG. 4 shows display 13 at 880 nanometers wavelength which can only be seen by the first viewer, and display 15 at 750 nanometers wavelength, which can only be seen by the second viewer .
In catadioptric area-of-interes t display (CA0ID) projection systems, with two viewers, such as the pilot and weapons system officer of a jet fighter simulator, simultaneously present during a night-viewing simulation, each wears viewing means, such as night-vision goggles to amplify the dim light to usable levels. Sensors determine the direction that each viewer's goggles are pointing, and generate one or more signals to direct simultaneously one area-of-interest display into the field of view of one viewer, another display into the field of view of the other .
As illustrated in FIG. 4, CA0ID projection system 1 has a plurality of image inputs to beamsplitter 6. Computer image generator channels A and B produce image sources 40 and 42, respectively, which may be devices that convert electrical video signals to spatially modulated displays at the desired wavelength. Light from image source 42 travels on path 43 to relay telescope 44 and, from telescope 44, on path 4 , to beam splitter 6. The light from source 42 is directed by motor driven mirror 48 into the optics of projection system 1. Similarly, 97246/2 light from image source 40 travels on path 49 to relay telescope 50. Light emerging from relay telescope 50 on path 5 is directed by motor driven mirror 1 to beamsplitter 6 for combination with the light entering from path 4 · The combined images are then directed along path to eyepiece/mirror assembly 24 and, from there, along path 55 into opening 23 of dome 22 . Inside dome 22 , the image from source 42 is displayed on dome surface area 56 and the image from source 40 on dome surface area 57 simultaneously.
To prevent the pilot and the weapons system officer from seeing the display intended for the other viewer, each viewer's goggles include a filter for each eye to reject incident light that originates with the display intended for the other viewer, and to transmit only the light from the display intended for him.
Independent, non-interfering displays also prevent perspective distortion, which depends on the finite distance from each viewer to the display, for example, assuming the use of a two-position fighter simulator inside a 30-foot diameter dome, one viewer may have perspective distortion error up to 20 degrees if he sees the display intended for the other viewer. The viewing means of the invention permit this problem to be solved by image distortion correction techniques uniquely tailored for each observer .
A complete description of these CAOID devices appears in U.S. Patent No. 5 , 004,331, entitled ' Catadioptric Projector, Catadioptric Projection System and Process,' the disclosure of which is incorporated herein by this reference.

Claims (6)

97246/3 C L A I S
1. A complementary viewing system for a first and second viewer simultaneously using said system comprising: means for directing a first image toward the first viewe ; means for simultaneously directing a second image toward the second viewer, said first image being at least partially in the field of view of the second viewer and the second image being at least partially in the field of view of the first viewer; first selective light transmitting means positioned in the path of the images directed toward said first viewer, with radiance at substantially only a first predetermined wavelength, rejecting or absorbing substantially all radiance at substantially all other wavelengths; and second selective light transmitting means positioned in the path of the images directed toward said second viewer, said second selective light transmitting means for transmitting the second image to the second viewer, the second image with radiance at substantially only a second predetermined wavelength, for rejecting or absorbing substantially all radiance at substantially all other wavelengths.
2. The system of claim 1, wherein said first and second wavelengths are infrared. 97246/2
3. The system of claim 1 wherein said viewing system includes catadioptric area of interest displays.
4. The system of claim 1 wherein said first transmitting means is a filter.
5. The system of claim 1 wherein said second transmitting means is selected from the group consisting of a single holographic element, multiple holographic elements, or thin films .
6. The system of claim 4 wherein said first means comprises goggles. 7· The system of claim 4 wherein said second means comprises goggles. For the Applicant, & Co.
IL9724691A 1990-02-20 1991-02-14 Non-interfering viewing system for use in catadioptric projection systems IL97246A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US48154890A 1990-02-20 1990-02-20

Publications (2)

Publication Number Publication Date
IL97246A0 IL97246A0 (en) 1992-05-25
IL97246A true IL97246A (en) 1994-05-30

Family

ID=23912379

Family Applications (1)

Application Number Title Priority Date Filing Date
IL9724691A IL97246A (en) 1990-02-20 1991-02-14 Non-interfering viewing system for use in catadioptric projection systems

Country Status (5)

Country Link
EP (1) EP0443793B1 (en)
JP (1) JPH04215646A (en)
DE (1) DE69126454T2 (en)
IL (1) IL97246A (en)
TW (1) TW198748B (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA2264887A1 (en) * 1996-09-09 1998-03-19 Imax Corporation Method and apparatus for presenting a visual display to an audience
DE102004052102A1 (en) * 2004-10-26 2006-05-04 Rheinmetall Defence Electronics Gmbh vision system

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB906042A (en) * 1957-09-23 1962-09-19 General Precision Systems Ltd Improvements in or relating to optical apparatus for creating the illusion of movement in simulated vehicles
US3917399A (en) * 1974-10-02 1975-11-04 Tropel Catadioptric projection printer
US4106855A (en) * 1975-08-13 1978-08-15 Martin Marietta Corporation Lens element incorporating narrow bandpass filter and usable in dual mode
DE2702496A1 (en) * 1976-02-12 1977-08-18 Xerox Corp Catadioptric lens for electrostatic copier - incorporates dichroic filter for blue light for better reproduction of blue matter on white background
US4134644A (en) * 1977-01-10 1979-01-16 Marks Alvin M 3D Color pictures with multichrome filters
FR2393332A2 (en) * 1977-06-01 1978-12-29 Instruments Sa REFLECTIVE LENS
GB1574351A (en) * 1978-02-27 1980-09-03 Smiths Industries Ltd Display apparatus
US4500163A (en) * 1981-07-29 1985-02-19 The Singer Company Holographic projection screen
HU193030B (en) * 1982-09-14 1987-08-28 Istvan Kalocsai Optical instrument of wide visual angle
US4620770A (en) * 1983-10-25 1986-11-04 Howard Wexler Multi-colored anaglyphs
US4671603A (en) * 1983-11-17 1987-06-09 Pilkington P.E. Limited Optical filters and multiplexing-demultiplexing devices using the same
US4834515A (en) * 1984-11-29 1989-05-30 Lockheed Missiles & Space Company, Inc. Catadioptric imaging system with dioptric assembly of the petzval type
US4657512A (en) * 1985-06-08 1987-04-14 The Singer Company Visual system with filter for a simulator
US5004331A (en) * 1989-05-03 1991-04-02 Hughes Aircraft Company Catadioptric projector, catadioptric projection system and process

Also Published As

Publication number Publication date
IL97246A0 (en) 1992-05-25
EP0443793B1 (en) 1997-06-11
EP0443793A2 (en) 1991-08-28
DE69126454D1 (en) 1997-07-17
TW198748B (en) 1993-01-21
JPH04215646A (en) 1992-08-06
DE69126454T2 (en) 1997-12-04
EP0443793A3 (en) 1992-08-19

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